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VALEMA SIGNED

VALidation tests of ElectroMechanical Actuators and its dedicated control units at TRL 6 level

Total Cost €

0

EC-Contrib. €

0

Partnership

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Project "VALEMA" data sheet

The following table provides information about the project.

Coordinator
GMV AEROSPACE AND DEFENCE SA 

Organization address
address: CALLE ISAAC NEWTON PARQUE TECNOLOGICO DE MADRID
city: TRES CANTOS
postcode: 28760
website: n.a.

contact info
title: n.a.
name: n.a.
surname: n.a.
function: n.a.
email: n.a.
telephone: n.a.
fax: n.a.

 Coordinator Country Spain [ES]
 Total cost 1˙091˙512 €
 EC max contribution 782˙512 € (72%)
 Programme 1. H2020-EU.3.4.5.6. (ITD Systems)
 Code Call H2020-CS2-CFP04-2016-02
 Funding Scheme CS2-IA
 Starting year 2017
 Duration (year-month-day) from 2017-06-01   to  2022-07-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    GMV AEROSPACE AND DEFENCE SA ES (TRES CANTOS) coordinator 260˙137.00
2    RAMEM SA ES (MADRID) participant 230˙125.00
3    UMBRAGROUP SPA IT (FOLIGNO PG) participant 170˙625.00
4    FUNDACION TECNALIA RESEARCH & INNOVATION ES (DERIO BIZKAIA) participant 61˙512.00
5    SKYLIFE ENGINEERING SL ES (SEVILLA) participant 60˙112.00

Map

 Project objective

The objective of the VALEMA project is twofold: - On the one hand it is required to manufacture and assembly units (EMAs and ECUs) previously designed and developed according to the JTI-CS2-2016-CFP03-SYS-02-14 Call (Development of electromechanical actuators and electronic control units for flight control systems) for in flight tests activities. - On the other hand it is required to perform certification activities regarding both the HW and SW of the ECUs in order to obtain a permit to fly in the FTB2 demonstrator of the Regional Aircraft.

The manufacturing part will include a deep analysis of manufacturing routes, materials to be used and applicable qualification tests, searching for innovative processes, in order to ensure that the processes optimize the manufacturing time, minimize the raw material used and minimize the environmental impact.

The certification activities will be aimed at obtaining the permit to fly from the applicable Airworthiness Authorities for the aileron/spoiler ECU HW design (according to DO-254) and for the aileron/spoiler ECU SW design (according to DO-178B).

These activities can be considered as the last step within the HW and SW design of the aileron/spoiler ECU development to be undertaken in EMA4FLIGHT according to the JTI-CS2-2016-CFP03-SYS-02-14 Call and, as such, the innovations developed within that call also apply herein.

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The information about "VALEMA" are provided by the European Opendata Portal: CORDIS opendata.

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